View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 59661U 26145.51088142 +.00000000 +00000-0 +10404-3 0 00009
2 59661 42.9992 324.3513 0001321 268.5445 91.5255 15.27583327 06
| Epoch (UTC): | 25 May 2026 12:15:40 |
| Eccentricity: | 0.0001321 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.3513° |
| argument of perigee: | 268.5445° |
| revolutions per day: | 15.27583327 |
| mean anomaly at epoch: | 91.5255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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